View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 43930U 19002J 24358.14223602 .00001951 00000-0 30547-3 0 9991
2 43930 86.6108 219.6748 0002328 84.2782 275.8701 14.72257941319659
| Epoch (UTC): | 23 December 2024 03:24:49 |
| Eccentricity: | 0.0002328 |
| inclination: | 86.6108° |
| perigee height: | 652 km |
| apogee height: | 655 km |
| right ascension of ascending node: | 219.6748° |
| argument of perigee: | 84.2782° |
| revolutions per day: | 14.72257941 |
| mean anomaly at epoch: | 275.8701° |
| orbit number at epoch: | 31965 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|